A method for enhancing the characteristics of ultra-high-speed impact damage area

A technology of ultra-high-speed impact and regional features, applied in image enhancement, image analysis, instruments, etc., can solve the problems of low computational efficiency and universality of algorithms, and inability to guarantee the segmentation quality of infrared reconstructed images

Active Publication Date: 2022-03-18
中国空气动力研究与发展中心超高速空气动力研究所
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Problems solved by technology

If only the segmentation model is used, the weight coefficients corresponding to the objective functions to achieve the three segmentation performances when forming the segmentation function are to be determined, and continuous debugging is required to determine the weight coefficients to control the balance between each objective function, and the computational efficiency and universality of the algorithm The performance is low, and the segmentation quality of the final infrared reconstructed image cannot be guaranteed

Method used

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  • A method for enhancing the characteristics of ultra-high-speed impact damage area
  • A method for enhancing the characteristics of ultra-high-speed impact damage area
  • A method for enhancing the characteristics of ultra-high-speed impact damage area

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Embodiment

[0178] In this embodiment, the infrared thermal imaging camera collected 502 frames of images with a pixel size of 512×640. That is, there are 327,680 temperature points on each map, and the temperature value of each temperature point is recorded 502 times. This time-varying temperature condition constitutes the transient thermal response TTR of the temperature point. Step 1: After extracting the effective transient thermal response from the infrared thermal sequence, divide the area according to the defect type, and extract the typical transient thermal response from each type of divided area. When extracting the effective transient thermal response, set the parameter ReCL =0.92, 441 valid transient thermal responses containing complete defect information were extracted from 327,680 temperature points. According to the pixel points, the membership degree of each cluster center is softened, and 12, 251 and 178 thermal response curves are divided into corresponding categories...

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Abstract

The invention discloses a method for enhancing the characteristics of an ultra-high-speed impact damage area, which includes: extracting a typical transient thermal response of a defect; obtaining an infrared reconstruction image; separating the background area and the defect area of ​​the infrared reconstruction image; removing noise, The infrared image segmentation function is constructed under the guidance of the purpose of preserving details and edges; the multi-objective optimization algorithm combined with the segmentation model realizes one-time segmentation of the specimen defects in the infrared reconstructed image; according to the distance from the pixel point in the infrared image to the cluster center, the The pixels are divided into categories to obtain the segmented image of the damage defect in the infrared detection image. The invention utilizes multi-objective optimization theory to segment defects in infrared reconstructed images, constructs objective functions respectively for noise problems and edge blur problems, improves the segmentation accuracy of damaged defect areas, has high defect detection rate, low false detection rate, and bulge enhancement The ultra-high-speed impact damage defect area in the infrared reconstruction image is identified, which is convenient for the quantitative study of complex defects.

Description

technical field [0001] The invention belongs to the technical field of spacecraft maintenance support and on-orbit risk assessment, and more specifically, the invention relates to a method for enhancing the characteristics of a hypervelocity impact damage area. Background technique [0002] During launch and in-orbit operation, spacecraft are extremely vulnerable to accidental impacts from various tiny objects, such as space junk fragments, tiny meteoroids, and peeled off coatings. In particular, the ever-increasing space junk debris is the most harmful to on-orbit spaceflight. Because the tiny debris has a very high impact speed (usually reaching several kilometers per second or even tens of kilometers per second), it is easy to cause various types of debris on the surface of the spacecraft. Hypervelocity impact damage, such as perforation, impact crater, spallation, spalling, etc., causes the structure of the spacecraft to be damaged or the function of the component to dec...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06T7/00G06T7/11G06T7/194G06T5/00G06V10/762G06V10/764G06K9/62
CPCG06T7/0004G06T7/11G06T7/194G06T5/002G06T2207/10048G06T2207/20192G06T2207/30108G06F18/23G06F18/24
Inventor 黄雪刚雷光钰谭旭彤石安华罗庆覃金贵赵君尧
Owner 中国空气动力研究与发展中心超高速空气动力研究所
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